General Description:
The test system provides the general electrical test equipment
necessary to test the spacecraft during subsystem and system level
integration and test operations as well as support the launch site
operation of the spacecraft. Slightly different configurations of
the system will be used for each stage of this testing. The
operator interacts with the test system for the control of the
electrical test equipment. Output of the test system is in the
form of print out as well as electronic data passed to the secure
system for analysis and archive purposes. Raw data from the test
system will also be stored locally for a time, and then pushed to
an offline archive media. Features:
The Guidance Navigation and Control subsystem provides the
equipment used to support satellite GN&C subsystem, On-Board
Computer software, Interface, Open-Loop and Closed-Loop stability
testing in satellite level test environments.
A typical GN&C subsystem interfaces consists the followings: